Similarly shaped airfoils to SB96 11.6/3.0
New! Bulk download of polars in Excel format: SB96%2011.6_3.0.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (0) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Basic Data: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl | Curve fits | Lift curve slopes
Data source comparison (Codes, CFD, Wind tunnel)
Compressibility Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Roughness Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Plain Flap Effects: cl,max vs flap deflection: all flap chords | 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cl vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cm vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cd vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. EM J18 3212
3. EM L3 3012
4. NACA63-612
5. SBC3
6. HQ 3.0/11
7. MID 343
8. HQ 3.0/12
9. NACA63-512 a=0.8
10. NACA63-611
11. NACA64-612
12. K3311 (smoothed)
13. EPPLER 853
14. MS3,3-11GP
15. EPPLER 201
16. K3311 (original)
17. NACA63-511 a=0.8
18. NACA63A511
19. NACA64-512 a=0.8
20. SB96 10.5/3.0
21. SB 96 12.7/3.0